Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine

Title
Development of a Throughflow-Based Simulation Tool for Preliminary Compressor Design Considering Blade Geometry in Gas Turbine Engine
Authors
Keywords
-
Journal
Applied Sciences-Basel
Volume 11, Issue 1, Pages 422
Publisher
MDPI AG
Online
2021-01-04
DOI
10.3390/app11010422

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